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| Question on typical numbers for rockets | 31 Jul 2004 22:48 GMT | 1 |
I'm playing with fantasy rockets for science fiction scenarios, and I'm looking for some typical figures for rockets. What would you say was a reasonable number for the following? # volume flow rate
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| X-Prize Design Concepts | 31 Jul 2004 04:48 GMT | 13 |
Afternoon all. The current foremost contender for the X-Prize is, of course, Scaled Composites - expected to formally announce soon, I believe - which uses a staged flight method, with horizontal takeoff and landing.
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| Elementary Bulk Metallic Glass | 26 Jul 2004 22:49 GMT | 5 |
Check out this article: http://www.e4engineering.com/story.aspx?nid=tsj5d&id=217987 Apparently, some researchers have found a way to turn pure Zirconium into a bulk metallic glass by using tremendous pressure. Right now, it
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| Could a bullet be made of something that could go from orbit to Earth's surface? | 26 Jul 2004 18:18 GMT | 17 |
I'm up on the Space Station and I go out for a nice little space walk. I take along my specially designed hunting rifle and fire a bullet down at the planet. What would the bullet need to be made of for it to make it all the way to the surface and not burn up on entry to our ...
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| heat shield testing | 26 Jul 2004 17:24 GMT | 1 |
How are thermal protection systems tested on the ground? By directing superheated air at various temperatures, pressures, and durations to simulate a re-entry environment?
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| Plane change using aerobraking | 26 Jul 2004 13:28 GMT | 2 |
In one of those moments of conceptual flux, I wondered if it would be feasible, using today's existing materials, to developp a zero-propellant orbital plane change capable satellite. (Emphasis on the word -propellant-, not -energy- ;-P)
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| On-Orbit Refueling Question | 24 Jul 2004 14:13 GMT | 5 |
Hey guys, I've been lurking for a while due to trying to get my thesis done and other things, but I had a quick question for the board. I already sent email to Henry and George, but figured I'd put it out for others too.
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| SpaceShip 1, 2 ..n | 23 Jul 2004 22:26 GMT | 5 |
A lot of discussion on this and other groups orbits around the difficulty is scaling SS1 to an orbital vehicle. There has been a lot of discussion about Mr Rutan's skills when one transfers from subsonic airplanes to hypersonice space vehicles.
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| Air Ship To Space? | 23 Jul 2004 05:04 GMT | 3 |
A while ago I saw an idea for an "Airship To Space" on JP Aerospace's website. How does this work? They mentioned using electric rockets which have very low thrust.
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| Satellite orbit parallel to equatorial plane | 22 Jul 2004 17:30 GMT | 9 |
I have two questions to ask: 1- Is it possible to have a satellite orbit parallel to the equatorial plane? Something like a GEO orbit but shifted up or down to cover other locations of the earth futher up from the equator. Such an
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| Is Titan's atmosphere biogenic in origin? | 22 Jul 2004 06:57 GMT | 6 |
Titan is unique among all the planetary moons in having a dense atmosphere. This atmosphere has a number of unusual characteristics that it shares with Earth's atmosphere, and which I think are consistent with it being biogenic.
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| SpaceShipOne and reentry heat | 21 Jul 2004 19:12 GMT | 33 |
I'm just an average person with an English degree, so I'm unfamiliar with the science and physics and space craft reentry, so this is likely a very stupid question. But it's my uneducated understanding that returning space craft, like
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| Inverted Aerobraking - a suggestion for a different way of propulsion for CATS in medium to far future | 21 Jul 2004 17:30 GMT | 3 |
Some months ago I reconsidered an old idea of mine about a different way to go to space. I still believe it might work. But feel free to tell me why you reckon it won't. Or maybe you have an idea how to use this concept better/simpler/more economical?
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| Altitude compensation with gas injection | 17 Jul 2004 21:55 GMT | 5 |
Suppose you have a high-altitude rocket nozzle: It expands the flow to << 1 psi at exit. Now suppose you want to light this thing off on the ground. You have an overexpanded nozzle, and you may get unpredictable flow seperation and you will get Isp losses from the flow to ambient
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| Spacex RP-1 Question... | 17 Jul 2004 21:24 GMT | 3 |
In reading Spacex's on line documents/updates I read that the RP-1 and LOX tanks share a common bulkhead. How do you keep the RP1 from turning to wax at LOX temperatures? Even if this bulkhead is insulated, how do you keep the common Al outer tank wall from
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